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> FC-1/JF-17
FC-1 (JF-17) Multirole Fighter Aircraft
Summary
Specifications
Last updated: 3 November 2007
Early Designation
Super-7
Official Designation
Fighter China-1 (FC-1)
PAF Designation
Joint Fighter-17 (JF-17) 'Thunder'
Function
Air-superiority; ground attack
Operator
Pakistani Air Force
Designer
Chengdu Aircraft Design Institute (611 Institute)
Contractor
Chengdu Aircraft Industry (Group) Corporation Ltd. (CAC)
Maiden Flight
25 August 2003
Crew
One
Estimated Cost
US$15~20 million
Length
14m
Wingspan
9m
Wing Area
5.1m
Canard Area
N/A
Empty Weight
6,320kg
Normal Take-off Weight
9,100kg
Max Take-off Weight
12,700kg
Fuel Capacity
2,300kg
Max Payload
3,700kg
Powerplant
1X Russian RD-93 turbofan
Thrust (dry)
49.4kN
Thrust (afterburning)
81.4kN
Max Level Speed
Mach 1.6~1.8 (high altitude)
Max Climb Rate
N/A
Service Ceiling
16,700m
Range
3,000km
Operational Radius
1,350km
In-flight refuelling
No
G limit
-3 ~ +8.5
Fixed Weapon
23mm or 30mm single-barrel cannon
External Hardpoints
Seven (1 under the fuselage centerline; 4 under the wings; 2 on the wingtips)
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